東華大學圖書館 |

Language: English

Help

回圖書館首頁

手機版館藏查詢

Back

Switch To: Labeled | MARC Mode | ISBD

Space Access Systems Design: Synthes...

Rana, Loveneesh.

Linked to FindBook

Google Book

Amazon

博客來

Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems./
Author:	Rana, Loveneesh.
Published:	Ann Arbor : ProQuest Dissertations & Theses, : 2017,
Description:	240 p.
Notes:	Source: Dissertation Abstracts International, Volume: 79-09(E), Section: B.
Contained By:	Dissertation Abstracts International79-09B(E).
Subject:	Aerospace engineering. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10833442
ISBN:	9780355912395

Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems.
Rana, Loveneesh.

Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems. - Ann Arbor : ProQuest Dissertations & Theses, 2017 - 240 p.

Source: Dissertation Abstracts International, Volume: 79-09(E), Section: B.

Thesis (Ph.D.)--The University of Texas at Arlington, 2017.

This item is not available from ProQuest Dissertations & Theses.

The early Conceptual Design (CD) of a Space Access System (SAS) is the most abstract, innovative, and technologically challenging phase throughout the entire aerospace product development life-cycle. While it is the most important life-cycle phase which influences around 80 percent of the overall life-cycle-cost, it is also the least understood design phase. The history of space access vehicle design provides numerous examples of projects that failed due to lack of a proper technology-hardware-mission assessment in the CD phase. The present dissertation addresses this crucial phase and develops a prototype best practice solution process to advance the current state of the art of the CD oriented vehicle design synthesis systems. The solution is a generic process that can be applied to all categories of the SAS. The Vertical-Takeoff Horizontal-Landing type SAS is selected as the demonstration case-study for the solution process. The research provides a proof of concept for how the proposed prototype solution process expands the scope and application of current applications of the CD assessment vertically across the SAS system`s hierarchy and horizontally across the life-cycle phases of the SAS.

ISBN: 9780355912395Subjects--Topical Terms:

1002622
Aerospace engineering.

Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems.
LDR:02317nmm a2200325 4500 001 2166002
005 20181203094031.5
008 190424s2017 ||||||||||||||||| ||eng d
020 $a 9780355912395
035 $a (MiAaPQ)AAI10833442
035 $a (MiAaPQ)2502vireo:908Rana
035 $a AAI10833442
040 $a MiAaPQ $c MiAaPQ
100 1 $a Rana, Loveneesh. $3 3354104
245 1 0 $a Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2017
300 $a 240 p.
500 $a Source: Dissertation Abstracts International, Volume: 79-09(E), Section: B.
500 $a Adviser: Bernd Chudoba.
502 $a Thesis (Ph.D.)--The University of Texas at Arlington, 2017.
506 $a This item is not available from ProQuest Dissertations & Theses.
520 $a The early Conceptual Design (CD) of a Space Access System (SAS) is the most abstract, innovative, and technologically challenging phase throughout the entire aerospace product development life-cycle. While it is the most important life-cycle phase which influences around 80 percent of the overall life-cycle-cost, it is also the least understood design phase. The history of space access vehicle design provides numerous examples of projects that failed due to lack of a proper technology-hardware-mission assessment in the CD phase. The present dissertation addresses this crucial phase and develops a prototype best practice solution process to advance the current state of the art of the CD oriented vehicle design synthesis systems. The solution is a generic process that can be applied to all categories of the SAS. The Vertical-Takeoff Horizontal-Landing type SAS is selected as the demonstration case-study for the solution process. The research provides a proof of concept for how the proposed prototype solution process expands the scope and application of current applications of the CD assessment vertically across the SAS system`s hierarchy and horizontally across the life-cycle phases of the SAS.
590 $a School code: 2502.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Systems science. $3 3168411
650 4 $a Mechanical engineering. $3 649730
690 $a 0538
690 $a 0790
690 $a 0548
710 2 $a The University of Texas at Arlington. $b Mechanical and Aerospace Engineering. $3 3286584
773 0 $t Dissertation Abstracts International $g 79-09B(E).
790 $a 2502
791 $a Ph.D.
792 $a 2017
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10833442